JP3805833B2 - 超音速及び／又は極超音速飛行用航空機のラムジェットエンジン - Google Patents

超音速及び／又は極超音速飛行用航空機のラムジェットエンジン Download PDF

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Publication number
JP3805833B2
JP3805833B2 JP18216596A JP18216596A JP3805833B2 JP 3805833 B2 JP3805833 B2 JP 3805833B2 JP 18216596 A JP18216596 A JP 18216596A JP 18216596 A JP18216596 A JP 18216596A JP 3805833 B2 JP3805833 B2 JP 3805833B2
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JP
Japan
Prior art keywords
ramjet engine
fluid
plate
wall
movable
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
JP18216596A
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English (en)
Japanese (ja)
Other versions
JPH0932641A (ja
Inventor
アラン・シュバリエ
マルク・ブッシェ
ヴァディム・ルヴィンヌ
ヴァレリー・アブラシコフ
ディミトリ・ダヴィデンコ
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Aerospatiale Matra
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Aerospatiale Matra
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
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Publication date
Application filed by Aerospatiale Matra filed Critical Aerospatiale Matra
Publication of JPH0932641A publication Critical patent/JPH0932641A/ja
Application granted granted Critical
Publication of JP3805833B2 publication Critical patent/JP3805833B2/ja
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/78—Other construction of jet pipes
    • F02K1/80—Couplings or connections
    • F02K1/805—Sealing devices therefor, e.g. for movable parts of jet pipes or nozzle flaps
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
    • F02K7/10—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fuel-Injection Apparatus (AREA)
  • Output Control And Ontrol Of Special Type Engine (AREA)
  • Physical Or Chemical Processes And Apparatus (AREA)
  • Nozzles (AREA)
JP18216596A 1995-07-13 1996-07-11 超音速及び／又は極超音速飛行用航空機のラムジェットエンジン Expired - Lifetime JP3805833B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR9508496 1995-07-13
FR9508496A FR2736685B1 (fr) 1995-07-13 1995-07-13 Statoreacteur pour aeronef a vol supersonique et/ou hypersonique

Publications (2)

Publication Number Publication Date
JPH0932641A JPH0932641A (ja) 1997-02-04
JP3805833B2 true JP3805833B2 (ja) 2006-08-09

Family

ID=9480967

Family Applications (1)

Application Number Title Priority Date Filing Date
JP18216596A Expired - Lifetime JP3805833B2 (ja) 1995-07-13 1996-07-11 超音速及び／又は極超音速飛行用航空機のラムジェットエンジン

Country Status (8)

Country Link
US (1) US5722234A (fr)
EP (1) EP0753654B1 (fr)
JP (1) JP3805833B2 (fr)
CA (1) CA2180501C (fr)
DE (1) DE69607691T2 (fr)
ES (1) ES2145399T3 (fr)
FR (1) FR2736685B1 (fr)
RU (1) RU2117807C1 (fr)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2476705C1 (ru) * 2011-11-17 2013-02-27 Федеральное государственное унитарное предприятие "Центральный институт авиационного моторостроения имени П.И. Баранова" Пульсирующий детонационный прямоточный воздушно-реактивный двигатель и способ функционирования двигателя
US20140364291A1 (en) * 2011-12-30 2014-12-11 Philip Morris Products S.A. Apparatus and method for supplying a continuous web of crimped sheet material
RU178988U1 (ru) * 2017-09-21 2018-04-24 Общество с ограниченной ответственностью "ВНХ-Механика" Сверхзвуковой прямоточный воздушно-реактивный двигатель
FR3072908B1 (fr) * 2017-10-26 2021-02-26 Safran Nacelles Ensemble propulsif pour aeronef

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4081137A (en) * 1977-01-05 1978-03-28 The United States Of America As Represented By The Secretary Of The Air Force Finned surface cooled nozzle
US4895378A (en) * 1988-06-15 1990-01-23 The Boeing Company Slidable high-temperature seal
US4930309A (en) * 1988-11-03 1990-06-05 Fleck Aerospace Limited Partnership Gas compressor for jet engine
DE4012212A1 (de) * 1990-04-14 1991-10-24 Mtu Muenchen Gmbh Duese fuer ein hyperschalltriebwerk
US5214914A (en) * 1990-04-30 1993-06-01 The Johns Hopkins University Translating cowl inlet with retractable propellant injection struts
US5076590A (en) * 1990-11-26 1991-12-31 The United States Of America, As Represented By The Administrator Of The National Aeronautics And Space Administration High temperature, flexible pressure-actuated, brush seal

Also Published As

Publication number Publication date
FR2736685A1 (fr) 1997-01-17
ES2145399T3 (es) 2000-07-01
CA2180501C (fr) 2006-11-21
US5722234A (en) 1998-03-03
DE69607691D1 (de) 2000-05-18
EP0753654A1 (fr) 1997-01-15
CA2180501A1 (fr) 1997-01-14
DE69607691T2 (de) 2000-09-07
JPH0932641A (ja) 1997-02-04
FR2736685B1 (fr) 1997-09-12
RU2117807C1 (ru) 1998-08-20
EP0753654B1 (fr) 2000-04-12

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